Method for nozzle clamping force control

Claim 3

The method of claim 1 wherein the nozzle system includes a fluid pressure driven actuator system for varying said nozzles and said step of sensing the force includes sensing the pressure applied to the actuator system.

Claim 4

The method of claim 2 wherein said step of opening a source of pressure includes directing pressure from the actuator system as applied to vary nozzles to a pressure actuated valving system controlling flow from the source of pressure.

Claim 5

The method of claim 1 wherein said step of opening a source of pressure includes restricting the resulting flow to allow a minimum pressure bleed off from between the vanes and the rings.

Claim 6

The method of claim 1 wherein said step of directing flow includes receiving flow from the influent to the radial turbine as the source of pressure.

Claim 7

A nozzle clamping force control for a variable primary nozzle system on a radial turbine having mounting rings mounted for relative axial movement therebetween, nozzle vanes clamped between the mounting rings, and an actuator for pivoting said nozzle vanes, comprising cavities in the nozzle vane surfaces adjacent the rings; passages extending to said cavities; a source of pressure in communication with said passages; valve means for controlling flow from said source of pressure through said passages; valve control means for opening said valve means responsive to actuator force.

Claim 8

A nozzle clamping force control for a variable primary nozzle system on a radial turbine having mounting rings mounted for relative axial movement therebetween, nozzle vanes clamped between the mounting rings, and an actuator for pivoting said nozzle vanes, comprising cavities in the nozzle vane surfaces adjacent the rings; passages extending to said cavities; a source of pressure in communication with said passages; valve means for controlling flow from said source of pressure through said passages; valve control means for opening said valve means responsive to actuator force.

Claim 9

The control of claim 6 wherein said passages extending to said cavities include a first passage extending through a ring to a first said cavity and a second passage extending from said first cavity to a second said cavity.

Claim 10

The control of claim 6 wherein said source of pressure is the influent to the radial turbine.

Claim 11

A nozzle clamping force control for a variable primary nozzle system on a radial turbine having mounting rings mounted for relative axial movement therebetween, nozzle vanes clamped between the mounting rings and a fluid pressure driven actuator for pivoting said nozzle vanes, comprising cavities in the nozzle vane surfaces adjacent the rings; passages extending to said cavities; a source of pressure in communication with said passages; valve means for controlling flow from said source of pressure through said passages; a valve actuator operatively coupled with said valve means; and a pressure line from the fluid pressure driven actuator to said valve actuator, said valve actuator being fluid pressure actuated and having a preselected actuation pressure.

Claim 12

A nozzle clamping force control for a variable primary nozzle system on a radial turbine having mounting rings mounted for relative axial movement therebetween, nozzle vanes clamped between the mounting rings and a fluid pressure driven actuator for pivoting said nozzle vanes, comprising cavities in the nozzle vane surfaces adjacent the rings; passages extending to said cavities; a source of pressure in communication with said passages; valve means for controlling flow from said source of pressure through said passages; a valve actuator operatively coupled with said valve means; and a pressure line from the fluid pressure driven actuator to said valve actuator, said valve actuator being fluid pressure actuated and having a preselected actuation pressure.

Claim 15

The method of claim 10 wherein the nozzle system includes a fluid pressure driven actuator system for varying said nozzles and said step of sensing the force includes sensing the pressure applied to the actuator system.

Claim 16

The method of claim 11 wherein said step of opening a source of pressure includes directing pressure from the actuator system as applied to vary nozzles to a pressure actuated valving system controlling flow from the source of pressure.

Claim 17

The method of claim 10 wherein said step of directing pressure includes receiving pressure from the influent to the radial turbine as the source of pressure.

Claim 18

The method of claim 10 wherein said step of directing flow includes receiving reduced pressure from the nozzle discharge area of the turbine as the source of pressure.

Claim 19

A nozzle clamping force control for a variable primary nozzle system on a radial turbine having mounting rings mounted for relative axial movement therebetween, nozzle vanes clamped between the mounting rings, and an actuator for pivoting said nozzle vanes, comprising at least one cavity laterally positioned to the nozzle vanes; a passage extending to said cavity; a source of pressure in communication with said passage; valve means for controlling pressure from said source of pressure through said passage; valve control means for opening said valve means responsive to actuator force.

Claim 20

A nozzle clamping force control for a variable primary nozzle system on a radial turbine having mounting rings mounted for relative axial movement therebetween, nozzle vanes clamped between the mounting rings, and an actuator for pivoting said nozzle vanes, comprising at least one cavity laterally positioned to the nozzle vanes; a passage extending to said cavity; a source of pressure in communication with said passage; valve means for controlling pressure from said source of pressure through said passage; valve control means for opening said valve means responsive to actuator force.

Claim 21

The control of claim 15 wherein said cavity is on an opposite side of one of the mounting rings to the nozzle vanes.

Claim 22

The control of claim 16 further including a vent port extending through the clamping ring from the cavity to adjacent at least one nozzle vane.

Claim 23

The control of claim 17 further including a passageway through at least one nozzle vane in alignment with said vent port.

Claim 24

The control of claim 16, 17 or 18 wherein said source of pressure is an area of reduced pressure in the turbine.

Claim 25

The control of claim 19 wherein said area of reduced pressure is the nozzle discharge.

Claim 26

The control of claim 15 wherein said source of pressure is the influent to the radial turbine.

Claim 27

A nozzle clamping force control for a variable primary nozzle system on a radial turbine having mounting rings mounted for relative axial movement therebetween, nozzle vanes clamped between the mounting rings and a fluid pressure driven actuator for pivoting said nozzle vanes, comprising a cavity laterally positioned adjacent a mounting ring on a side opposite from the nozzle vanes; a passage extending to said cavity; a source of pressure in communication with said passage; a valve means for controlling flow from said source of pressure through said passage; a valve actuator operatively coupled with said valve means; and a pressure line from the fluid pressure driven actuator to said valve actuator, said valve actuator being fluid pressure actuated and having a preselected actuation pressure.

Claim 28

A nozzle clamping force control for a variable primary nozzle system on a radial turbine having mounting rings mounted for relative axial movement therebetween, nozzle vanes clamped between the mounting rings and a fluid pressure driven actuator for pivoting said nozzle vanes, comprising a cavity laterally positioned adjacent a mounting ring on a side opposite from the nozzle vanes; a passage extending to said cavity; a source of pressure in communication with said passage; a valve means for controlling flow from said source of pressure through said passage; a valve actuator operatively coupled with said valve means; and a pressure line from the fluid pressure driven actuator to said valve actuator, said valve actuator being fluid pressure actuated and having a preselected actuation pressure.